stator at an angle of 55° from the axial direction. Draw the velocity diagrams at the inlet and outlet of the rotor. Determine the blade-loading coefficient. Determine at what angles the relative velocity enters and leaves the rotor. Determine at what angle the absolute velocity enters the rotor. e) Draw the Moiller diagram of this axial compressor
Fig: 1
Fig: 2
Fig: 3
Fig: 4
Fig: 5
Fig: 6